What was found
(CAN) MULTIPLE CRACKS THROUGH KNIFE EDGE SEALS. THIS REPORT WILL ALSO BE SUBMITTED TO MFG IAW SEI-183 SECTION 72-32-7 PAGE 302. (TC NR 20070726004)
- Difficulty date
- July 26, 2007
- Submitted
- August 3, 2007
- Operation
- General aviation
- Engine
- Ge CT581402
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Seal
- Part number
- 4017T37P02
- Condition
- Cracked
- Location
- Compressor
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.